FR2868753B1 - SYSTEM PROVIDING A TOUCH WARNING OF THE EXISTENCE OF EXCEEDING SAFETY PARAMETERS IN A HELICOPTER - Google Patents

SYSTEM PROVIDING A TOUCH WARNING OF THE EXISTENCE OF EXCEEDING SAFETY PARAMETERS IN A HELICOPTER

Info

Publication number
FR2868753B1
FR2868753B1 FR0503621A FR0503621A FR2868753B1 FR 2868753 B1 FR2868753 B1 FR 2868753B1 FR 0503621 A FR0503621 A FR 0503621A FR 0503621 A FR0503621 A FR 0503621A FR 2868753 B1 FR2868753 B1 FR 2868753B1
Authority
FR
France
Prior art keywords
helicopter
existence
system providing
safety parameters
touch warning
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
FR0503621A
Other languages
French (fr)
Other versions
FR2868753A1 (en
Inventor
Randall A Greene
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safe Flight Instr Corp
Safe Flight Instrument Corp
Original Assignee
Safe Flight Instr Corp
Safe Flight Instrument Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Safe Flight Instr Corp, Safe Flight Instrument Corp filed Critical Safe Flight Instr Corp
Publication of FR2868753A1 publication Critical patent/FR2868753A1/en
Application granted granted Critical
Publication of FR2868753B1 publication Critical patent/FR2868753B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • F02C9/285—Mechanical command devices linked to the throttle lever
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/04—Initiating means actuated personally
    • B64C13/042—Initiating means actuated personally operated by hand
    • B64C13/0421—Initiating means actuated personally operated by hand control sticks for primary flight controls
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/04—Initiating means actuated personally
    • B64C13/10—Initiating means actuated personally comprising warning devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/56—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • G—PHYSICS
    • G08—SIGNALLING
    • G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
    • G08B6/00—Tactile signalling systems, e.g. personal calling systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/303—Temperature
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/303—Temperature
    • F05D2270/3032—Temperature excessive temperatures, e.g. caused by overheating
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/40—Type of control system
    • F05D2270/44—Type of control system active, predictive, or anticipative

Abstract

Dans un hélicoptère, un système d'avertissement tactile avertissant d'un dépassement comporte un manche à balai de pilotage et un dispositif d'avertissement tactile (26) fixé au manche à balai (24). Un ordinateur (34) et un clavier servent à introduire un profil de températures de sécurité et un thermocouple mesure la température de sortie de la turbine. Un comparateur compare la température réelle avec le profil de températures de sécurité et active le dispositif d'avertissement tactile lorsque la température réelle se retrouve à l'extérieur du profil de températures de sécurité afin d'avertir le pilote qu'il doit suspendre l'exécution du démarrage.In a helicopter, a tactile warning system for warning of overshoot includes a pilot joystick and a tactile warning device (26) attached to the joystick (24). A computer (34) and keyboard are used to enter a safety temperature profile and a thermocouple measures the outlet temperature of the turbine. A comparator compares the actual temperature with the safety temperature profile and activates the tactile warning device when the actual temperature is outside the safety temperature profile to warn the pilot to suspend the startup execution.

FR0503621A 2004-04-12 2005-04-12 SYSTEM PROVIDING A TOUCH WARNING OF THE EXISTENCE OF EXCEEDING SAFETY PARAMETERS IN A HELICOPTER Expired - Fee Related FR2868753B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/821,974 US7262712B2 (en) 2004-04-12 2004-04-12 Helicopter tactile exceedance warning system

Publications (2)

Publication Number Publication Date
FR2868753A1 FR2868753A1 (en) 2005-10-14
FR2868753B1 true FR2868753B1 (en) 2010-07-30

Family

ID=33435676

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0503621A Expired - Fee Related FR2868753B1 (en) 2004-04-12 2005-04-12 SYSTEM PROVIDING A TOUCH WARNING OF THE EXISTENCE OF EXCEEDING SAFETY PARAMETERS IN A HELICOPTER

Country Status (6)

Country Link
US (1) US7262712B2 (en)
CA (1) CA2479142C (en)
FR (1) FR2868753B1 (en)
GB (1) GB2413120B (en)
IT (1) ITPI20050036A1 (en)
RU (1) RU2381960C2 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7126496B2 (en) * 2004-09-30 2006-10-24 Safe Flight Instrument Corporation Tactile cueing system and method for aiding a helicopter pilot in making landings
US8626363B2 (en) * 2007-02-08 2014-01-07 Bell Helicopter Textron Inc. Aircraft feathering, flapping and rotor loads indicator
US8827207B2 (en) 2011-05-03 2014-09-09 Goodrich Corporation Ice protection system
US8730065B2 (en) 2012-03-22 2014-05-20 Lockheed Martin Corporation System and method for tactile presentation of information
US8552847B1 (en) 2012-05-01 2013-10-08 Racing Incident Pty Ltd. Tactile based performance enhancement system
FR3002273B1 (en) * 2013-02-20 2017-06-23 Snecma AVIONIC DEVICE FOR MONITORING A TURBOMACHINE
FR3021627B1 (en) * 2014-05-28 2016-06-10 Airbus Helicopters ALARM DEVICE FOR A TILT SIGNAL GYROVAN PILOT USING A "TRIM CYLINDER" CONNECTED TO A FLIGHT CONTROL MEMBER
US9580186B1 (en) 2015-08-28 2017-02-28 Safe Flight Instrument Corporation Helicopter tactile stall warning
US10802482B2 (en) * 2017-02-27 2020-10-13 Textron Innovations Inc. Reverse tactile cue for rotorcraft rotor overspeed protection
US10474237B2 (en) 2017-07-25 2019-11-12 Rolls-Royce Corporation Haptic feedback for rotary wing aircraft

Family Cites Families (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2819838A (en) * 1952-07-23 1958-01-14 Douglas K Warner Centrifugal compressors
GB747857A (en) * 1952-09-04 1956-04-18 William Wilfred Lyle Improvements in warning devices
US3145915A (en) * 1959-11-20 1964-08-25 Motcurs D Aviat Soc Nat D Etud Compressors for fluids
GB890248A (en) * 1960-09-19 1962-02-28 Safe Flight Instrument An aircraft alam providing a tactile warning signal
JPS5614519B1 (en) * 1971-04-06 1981-04-04
US3775745A (en) * 1972-02-03 1973-11-27 Mcpherson D Engine over-temperature warning system
GB1476402A (en) * 1975-05-23 1977-06-16 Maris J Warning devices
US4115755A (en) * 1976-06-11 1978-09-19 United Technologies Corporation Aerodynamic surface load sensing
US4114442A (en) * 1976-09-03 1978-09-19 Avicon Development Group Temperature monitoring system
US4420808A (en) * 1980-04-01 1983-12-13 United Technologies Corporation Multi-axis force stick, self-trimmed aircraft flight control system
US4575803A (en) * 1981-12-30 1986-03-11 Semco Instruments, Inc. Engine monitor and recorder
US4787053A (en) * 1981-12-30 1988-11-22 Semco Instruments, Inc. Comprehensive engine monitor and recorder
US4619110A (en) * 1983-07-13 1986-10-28 Moore M Samuel Helicopter engine warning or control system
US4908618A (en) * 1988-12-27 1990-03-13 The Boeing Company Abnormal start advisory system (ASAS) for aircraft engines
US5076517A (en) * 1989-08-14 1991-12-31 United Technologies Corporation Programmable, linear collective control system for a helicopter
US5101619A (en) * 1990-02-20 1992-04-07 United Technologies Corporation Method for correcting a hot start condition
US5479350A (en) * 1993-08-23 1995-12-26 B&D Instruments And Avionics, Inc. Exhaust gas temperature indicator for a gas turbine engine
US5463873A (en) * 1993-12-06 1995-11-07 Cool Fog Systems, Inc. Method and apparatus for evaporative cooling of air leading to a gas turbine engine
US5552711A (en) * 1994-11-10 1996-09-03 Deegan; Thierry Turbine engine imminent failure monitor
JP2877098B2 (en) * 1995-12-28 1999-03-31 株式会社日立製作所 Gas turbines, combined cycle plants and compressors
US5930990A (en) * 1996-05-14 1999-08-03 The Dow Chemical Company Method and apparatus for achieving power augmentation in gas turbines via wet compression
SG104914A1 (en) * 1997-06-30 2004-07-30 Hitachi Ltd Gas turbine
JPH11229898A (en) * 1998-02-19 1999-08-24 Mitsubishi Heavy Ind Ltd Start-up control device of gas turbine
US6002348A (en) * 1998-05-13 1999-12-14 Safe Flight Instrument Corporation Pilot's aid for detecting power lines
US5986582A (en) * 1998-06-24 1999-11-16 Safe Flight Instrument Corporation Helicopter rotor/engine warning system
US6002349A (en) * 1998-08-14 1999-12-14 Safe Flight Instrument Corporation Helicopter anti-torque limit warning device
US6422023B1 (en) * 1998-12-11 2002-07-23 Alliedsignal Inc. Turbine engine control with electronic and pneumatic governors
DE19902437C5 (en) * 1999-01-22 2017-01-12 General Electric Technology Gmbh Method and device for rapid startup and for rapid increase in output of a gas turbine plant
US6473708B1 (en) * 1999-12-20 2002-10-29 Bechtel Bwxt Idaho, Llc Device and method for self-verifying temperature measurement and control
US6695264B2 (en) * 2000-05-16 2004-02-24 Bell Helicopter Textron, Inc. Power lever tactile cueing system
US7098811B2 (en) 2002-03-21 2006-08-29 Bell Helicopter Textron Inc. Method and apparatus for tactile cueing of aircraft controls

Also Published As

Publication number Publication date
GB0422028D0 (en) 2004-11-03
CA2479142C (en) 2007-12-04
CA2479142A1 (en) 2005-10-12
US20050225456A1 (en) 2005-10-13
RU2381960C2 (en) 2010-02-20
GB2413120B (en) 2008-12-03
ITPI20050036A1 (en) 2005-10-13
RU2005110551A (en) 2006-10-20
US7262712B2 (en) 2007-08-28
GB2413120A (en) 2005-10-19
FR2868753A1 (en) 2005-10-14

Similar Documents

Publication Publication Date Title
FR2868753B1 (en) SYSTEM PROVIDING A TOUCH WARNING OF THE EXISTENCE OF EXCEEDING SAFETY PARAMETERS IN A HELICOPTER
WO2004075034A3 (en) Non main cpu/os based operational environment
CN105942678A (en) Method for judging whether bracelet is not worn on hand
CN106066765A (en) A kind of bracelet wears the system of judgement
Guevara et al. Heparin-induced transaminase elevations: a prospective study.
Turtay et al. Coagulopathy in multiple traumas
Dorokhov Somnology and occupational safety
Marasco et al. Designing the ambulatory endoscopy center.
Michalek et al. Levels of 2, 3, 7, 8-tetrachlorodibenzo-p-dioxin in 1,302 unexposed Air Force Vietnam-era veterans.
Böhm et al. Lack of protection from development of multiple melanomas by an injected melanocortin analogue in a combined high-risk MC1R/CDKN2A genotype patient.
Sundararajan et al. The rain check
Tamizhchelvi Projecting safety measures in fireworks factories in Sivakasi using fuzzy based approach
Saccavini et al. Integration of telehealth and telecare service in the Veneto region.
Kristensen et al. Airborne contact allergy provoked by kathon in water-based plastic paint
Wang et al. Designing and Realiztion of Information System Development Platform Based on XML
Nishi et al. Squamous cell metaplasia in the rectum: a case report and review of the medical literature.
Han Embedded System Design
Fan et al. Computer actualization of bulk carrier safety evaluation.
Litvinenko Character and dynamics of structural changes in the liver under the effects of low temperature
Jiang et al. Semi-analytical approach for calculating index of non-probabilistic reliability based on interval analysis.
Abakumova et al. NEW NUTRITION TECHNOLOGY IN THE CONDITIONS OF HARMFUL EFFECTS OF ENVIRONMENT.
Blirup-Jensen et al. A simple model for training basic laparoscopic skills
Berney et al. Evaluation of satisfaction of nurses: development and validation of a new analysis tool
Torre et al. Nursing Intervention Classification (NIC) and Nursing Outcome Classification (NOC,) of Iowa University: a description of methods, tools and contents
Gribble et al. Differentsirovannaya chuvstvitel'nost'?-kletochnykh i ekstrapankreaticheskikh ATF zavisimykh K kanalov k gliklazidu

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14

PLFP Fee payment

Year of fee payment: 16

ST Notification of lapse

Effective date: 20211205